EP2108785A3 - Ensemble d'aubes statoriques et rotoriques de turbine avec une plateforme en céramique - Google Patents

Ensemble d'aubes statoriques et rotoriques de turbine avec une plateforme en céramique Download PDF

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Publication number
EP2108785A3
EP2108785A3 EP09250851A EP09250851A EP2108785A3 EP 2108785 A3 EP2108785 A3 EP 2108785A3 EP 09250851 A EP09250851 A EP 09250851A EP 09250851 A EP09250851 A EP 09250851A EP 2108785 A3 EP2108785 A3 EP 2108785A3
Authority
EP
European Patent Office
Prior art keywords
turbine blade
vane assembly
ceramic platform
blades
turbine
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP09250851A
Other languages
German (de)
English (en)
Other versions
EP2108785B1 (fr
EP2108785A2 (fr
Inventor
Michael G. Mccaffrey
Eric A. Hudson
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by United Technologies Corp filed Critical United Technologies Corp
Priority to EP14161778.7A priority Critical patent/EP2752557B1/fr
Publication of EP2108785A2 publication Critical patent/EP2108785A2/fr
Publication of EP2108785A3 publication Critical patent/EP2108785A3/fr
Application granted granted Critical
Publication of EP2108785B1 publication Critical patent/EP2108785B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • F01D5/3015—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements
    • F01D11/006—Sealing the gap between rotor blades or blades and rotor
    • F01D11/008—Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/80—Platforms for stationary or moving blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
EP09250851.4A 2008-04-11 2009-03-25 Ensemble d'aubes statoriques et rotoriques de turbine avec une plateforme en céramique Active EP2108785B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP14161778.7A EP2752557B1 (fr) 2008-04-11 2009-03-25 Pâle de turbine sans plate-forme

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US12/101,326 US8408874B2 (en) 2008-04-11 2008-04-11 Platformless turbine blade

Related Child Applications (2)

Application Number Title Priority Date Filing Date
EP14161778.7A Division-Into EP2752557B1 (fr) 2008-04-11 2009-03-25 Pâle de turbine sans plate-forme
EP14161778.7A Division EP2752557B1 (fr) 2008-04-11 2009-03-25 Pâle de turbine sans plate-forme

Publications (3)

Publication Number Publication Date
EP2108785A2 EP2108785A2 (fr) 2009-10-14
EP2108785A3 true EP2108785A3 (fr) 2013-01-09
EP2108785B1 EP2108785B1 (fr) 2017-10-04

Family

ID=40846162

Family Applications (2)

Application Number Title Priority Date Filing Date
EP14161778.7A Active EP2752557B1 (fr) 2008-04-11 2009-03-25 Pâle de turbine sans plate-forme
EP09250851.4A Active EP2108785B1 (fr) 2008-04-11 2009-03-25 Ensemble d'aubes statoriques et rotoriques de turbine avec une plateforme en céramique

Family Applications Before (1)

Application Number Title Priority Date Filing Date
EP14161778.7A Active EP2752557B1 (fr) 2008-04-11 2009-03-25 Pâle de turbine sans plate-forme

Country Status (2)

Country Link
US (1) US8408874B2 (fr)
EP (2) EP2752557B1 (fr)

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US8262345B2 (en) * 2009-02-06 2012-09-11 General Electric Company Ceramic matrix composite turbine engine
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FR2962156B1 (fr) * 2010-07-02 2012-08-10 Snecma Roue mobile a aubes en materiau composite pour moteur a turbine a gaz a liaison pied d'aube/disque par visserie
FR2963383B1 (fr) 2010-07-27 2016-09-09 Snecma Aube de turbomachine, rotor, turbine basse pression et turbomachine equipes d'une telle aube
US20120156045A1 (en) * 2010-12-17 2012-06-21 General Electric Company Methods, systems and apparatus relating to root and platform configurations for turbine rotor blades
US10287897B2 (en) 2011-09-08 2019-05-14 General Electric Company Turbine rotor blade assembly and method of assembling same
WO2013144024A1 (fr) 2012-03-28 2013-10-03 Alstom Technology Ltd Procédé pour séparer une pièce métallique d'une pièce en céramique
WO2013144035A1 (fr) * 2012-03-28 2013-10-03 Alstom Technology Ltd Procédé de traitement d'un élément hybride modulaire
EP2644828A1 (fr) * 2012-03-29 2013-10-02 Siemens Aktiengesellschaft Aube de turbine modulaire avec plateforme
CN104411921A (zh) 2012-06-30 2015-03-11 通用电气公司 涡轮机叶片密封结构
US9239062B2 (en) * 2012-09-10 2016-01-19 General Electric Company Low radius ratio fan for a gas turbine engine
US9527262B2 (en) 2012-09-28 2016-12-27 General Electric Company Layered arrangement, hot-gas path component, and process of producing a layered arrangement
US20140161616A1 (en) * 2012-12-12 2014-06-12 United Technologies Corporation Multi-piece blade for gas turbine engine
US9453422B2 (en) 2013-03-08 2016-09-27 General Electric Company Device, system and method for preventing leakage in a turbine
US9759082B2 (en) 2013-03-12 2017-09-12 Rolls-Royce Corporation Turbine blade track assembly
EP2971588A1 (fr) 2013-03-13 2016-01-20 Rolls-Royce Corporation Système de retenue à queues d'aronde pour chemins d'aubes
JP6240786B2 (ja) 2013-09-11 2017-11-29 ゼネラル・エレクトリック・カンパニイ Ｃｍｃタービンブレードの一体のプラットフォーム及びダンパ保持特徴のためのプライ構造
EP3055509B1 (fr) 2013-10-11 2024-03-06 RTX Corporation Aube de turbine à gaz en matériau composite à matrice céramique avec une plate-forme et une queue d'aronde en céramique monolithique
JP6479328B2 (ja) * 2014-04-02 2019-03-06 三菱日立パワーシステムズ株式会社 動翼及び回転機械
JP2017530290A (ja) * 2014-08-22 2017-10-12 シーメンス エナジー インコーポレイテッド 別個のプラットフォーム支持システムを備えるモジュール式タービンブレード
US10280768B2 (en) 2014-11-12 2019-05-07 Rolls-Royce North American Technologies Inc. Turbine blisk including ceramic matrix composite blades and methods of manufacture
US9909430B2 (en) 2014-11-13 2018-03-06 Rolls-Royce North American Technologies Inc. Turbine disk assembly including seperable platforms for blade attachment
US20160186593A1 (en) * 2014-12-31 2016-06-30 General Electric Company Flowpath boundary and rotor assemblies in gas turbines
FR3032753B1 (fr) * 2015-02-16 2018-11-23 Safran Aircraft Engines Redresseur pour une turbomachine
US20160305260A1 (en) * 2015-03-04 2016-10-20 Rolls-Royce North American Technologies, Inc. Bladed wheel with separable platform
US10227880B2 (en) 2015-11-10 2019-03-12 General Electric Company Turbine blade attachment mechanism
US10584592B2 (en) * 2015-11-23 2020-03-10 United Technologies Corporation Platform for an airfoil having bowed sidewalls
US10294954B2 (en) 2016-11-09 2019-05-21 Rolls-Royce North American Technologies Inc. Composite blisk
US10358922B2 (en) 2016-11-10 2019-07-23 Rolls-Royce Corporation Turbine wheel with circumferentially-installed inter-blade heat shields
US10563665B2 (en) 2017-01-30 2020-02-18 Rolls-Royce North American Technologies, Inc. Turbomachine stage and method of making same
US10731487B2 (en) 2017-02-20 2020-08-04 General Electric Company Turbine components and methods of manufacturing
US10767498B2 (en) 2018-04-03 2020-09-08 Rolls-Royce High Temperature Composites Inc. Turbine disk with pinned platforms
US10577961B2 (en) 2018-04-23 2020-03-03 Rolls-Royce High Temperature Composites Inc. Turbine disk with blade supported platforms
US10890081B2 (en) 2018-04-23 2021-01-12 Rolls-Royce Corporation Turbine disk with platforms coupled to disk
US10677075B2 (en) 2018-05-04 2020-06-09 General Electric Company Composite airfoil assembly for an interdigitated rotor
US10941665B2 (en) 2018-05-04 2021-03-09 General Electric Company Composite airfoil assembly for an interdigitated rotor
US11131203B2 (en) 2018-09-26 2021-09-28 Rolls-Royce Corporation Turbine wheel assembly with offloaded platforms and ceramic matrix composite blades
US11261744B2 (en) 2019-06-14 2022-03-01 Raytheon Technologies Corporation Ceramic matrix composite rotor blade attachment
US11156110B1 (en) 2020-08-04 2021-10-26 General Electric Company Rotor assembly for a turbine section of a gas turbine engine
US11655719B2 (en) 2021-04-16 2023-05-23 General Electric Company Airfoil assembly

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US3694104A (en) * 1970-10-07 1972-09-26 Garrett Corp Turbomachinery blade
US4501053A (en) * 1982-06-14 1985-02-26 United Technologies Corporation Method of making rotor blade for a rotary machine
US5222865A (en) * 1991-03-04 1993-06-29 General Electric Company Platform assembly for attaching rotor blades to a rotor disk
WO2000057032A1 (fr) * 1999-03-24 2000-09-28 Siemens Aktiengesellschaft Aube directrice et couronne directrice pour turbomachine, et element pour limiter un canal d'ecoulement
EP1219787A1 (fr) * 2000-12-27 2002-07-03 Siemens Aktiengesellschaft Aube de turbine à gaz et turbine à gaz
US20050169759A1 (en) * 2004-02-02 2005-08-04 General Electric Company Gas turbine flowpath structure
US20070116575A1 (en) * 2005-11-22 2007-05-24 Siemens Power Generation, Inc. Turbine blade assembly and method of manufacture
US20070189901A1 (en) * 2003-03-22 2007-08-16 Dundas Jason E Separable blade platform

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US5030063A (en) * 1990-02-08 1991-07-09 General Motors Corporation Turbomachine rotor
US5240377A (en) * 1992-02-25 1993-08-31 Williams International Corporation Composite fan blade
US5310317A (en) * 1992-08-11 1994-05-10 General Electric Company Quadra-tang dovetail blade
DE19941134C1 (de) * 1999-08-30 2000-12-28 Mtu Muenchen Gmbh Schaufelkranz für eine Gasturbine
US6190131B1 (en) * 1999-08-31 2001-02-20 General Electric Co. Non-integral balanced coverplate and coverplate centering slot for a turbine
US7007382B2 (en) 2003-07-24 2006-03-07 United Technologies Corporation Slot machining
US6951447B2 (en) 2003-12-17 2005-10-04 United Technologies Corporation Turbine blade with trailing edge platform undercut
US7261518B2 (en) 2005-03-24 2007-08-28 Siemens Demag Delaval Turbomachinery, Inc. Locking arrangement for radial entry turbine blades
US7255536B2 (en) 2005-05-23 2007-08-14 United Technologies Corporation Turbine airfoil platform cooling circuit
US7300253B2 (en) 2005-07-25 2007-11-27 Siemens Aktiengesellschaft Gas turbine blade or vane and platform element for a gas turbine blade or vane ring of a gas turbine, supporting structure for securing gas turbine blades or vanes arranged in a ring, gas turbine blade or vane ring and the use of a gas turbine blade or vane ring
US7467924B2 (en) 2005-08-16 2008-12-23 United Technologies Corporation Turbine blade including revised platform
US7510379B2 (en) 2005-12-22 2009-03-31 General Electric Company Composite blading member and method for making
US7507466B2 (en) 2006-02-22 2009-03-24 General Electric Company Manufacture of CMC articles having small complex features
US7874804B1 (en) * 2007-05-10 2011-01-25 Florida Turbine Technologies, Inc. Turbine blade with detached platform

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3694104A (en) * 1970-10-07 1972-09-26 Garrett Corp Turbomachinery blade
US4501053A (en) * 1982-06-14 1985-02-26 United Technologies Corporation Method of making rotor blade for a rotary machine
US5222865A (en) * 1991-03-04 1993-06-29 General Electric Company Platform assembly for attaching rotor blades to a rotor disk
WO2000057032A1 (fr) * 1999-03-24 2000-09-28 Siemens Aktiengesellschaft Aube directrice et couronne directrice pour turbomachine, et element pour limiter un canal d'ecoulement
EP1219787A1 (fr) * 2000-12-27 2002-07-03 Siemens Aktiengesellschaft Aube de turbine à gaz et turbine à gaz
US20070189901A1 (en) * 2003-03-22 2007-08-16 Dundas Jason E Separable blade platform
US20050169759A1 (en) * 2004-02-02 2005-08-04 General Electric Company Gas turbine flowpath structure
US20070116575A1 (en) * 2005-11-22 2007-05-24 Siemens Power Generation, Inc. Turbine blade assembly and method of manufacture

Also Published As

Publication number Publication date
EP2108785B1 (fr) 2017-10-04
US8408874B2 (en) 2013-04-02
EP2108785A2 (fr) 2009-10-14
EP2752557B1 (fr) 2019-02-06
EP2752557A3 (fr) 2014-09-10
US20090257875A1 (en) 2009-10-15
EP2752557A2 (fr) 2014-07-09

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